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Étude d'un moyen d'essais permettant de tester des structures de fuselage double courbure

Other title
Text fixture for fuselage double curved panel (en)
Author
SAVES, Cyrille1 ; GERMES, Saint1
[1] COE Nose and Center Fuselage, Airbus-France, 316 route de Bayonne, 31060 Toulouse, France
Source

Mécanique & industries. 2008, Vol 9, Num 6, pp 477-485, 9 p ; ref : 5 ref

ISSN
1296-2139
Scientific domain
Mechanical engineering; Mechanics acoustics
Publisher
EDP Sciences, Les Ulis
Publication country
France
Document type
Article
Language
French
Author keyword
Facility compression double curvature finite element fuselage
Keyword (fr)
Aéronef Banc essai Bridage Double courbure Fuselage Modélisation Méthode élément fini Porte pièce
Keyword (en)
Aircraft Test bench Clamping Double curvature Fuselage Modeling Finite element method Work holder
Keyword (es)
Aeronave Banco prueba Apriete Doble curvatura Fuselaje Modelización Método elemento finito Portapieza
Classification
Pascal
001 Exact sciences and technology / 001B Physics / 001B40 Fundamental areas of phenomenology (including applications) / 001B40F Solid mechanics / 001B40F30 Structural and continuum mechanics / 001B40F30R Measurement and testing methods

Discipline
Physics : solid mechanics
Origin
Inist-CNRS
Database
PASCAL
INIST identifier
21453171

Sauf mention contraire ci-dessus, le contenu de cette notice bibliographique peut être utilisé dans le cadre d’une licence CC BY 4.0 Inist-CNRS / Unless otherwise stated above, the content of this bibliographic record may be used under a CC BY 4.0 licence by Inist-CNRS / A menos que se haya señalado antes, el contenido de este registro bibliográfico puede ser utilizado al amparo de una licencia CC BY 4.0 Inist-CNRS

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